Engine: 1 x LHTEC T800 turboshaft, driving both the coaxial rotor and the six-bladed pusher propeller Power 1000 – 1250 kW (1300 – 1680 shp)
Performance: Max. cruise speed (max.): 460 km/h (250 kts) Range 1300 km These may have changed.
Blades: Eagle Aviation Technologies is to provide the blades. http://www.eagleaviationtech.com/
Propeller: Aero Composites, Inc. will build the six-bladed propulsor. http://www.aerocomposites.com/
Fly-by-Wire: These technologies include an integrated Fly-by-Wire system that allows the engine/rotor/propulsor system to operate efficiently, with full control of rotor rpm throughout the flight envelope, I.e. Variable speed rotors.
The Sikorsky X2 TECHNOLOGY™ demonstrator aircraft will incorporate several new technologies and demonstrate them in a flight environment. These technologies include an integrated Fly-by-Wire system that allows the engine/rotor/propulsor system to operate efficiently, with full control of rotor rpm throughout the flight envelope, high lift-to-drag rigid blades, low drag hub fairings, and Active Vibration Control. In addition, the aircraft will be used as a ‘flying wind tunnel’ to determine the main rotor to propulsor aerodynamic interaction, shaft angle optimization for performance, and blade tip clearance for a range of maneuvers. This will allow optimization of the X2 TECHNOLOGY™ suite for future products.
Sikorsky Aircraft reports that it has successfully ground tested the drive and pitch control for the six-bladed pusher propeller behind its high-speed X2 advancing blade concept (ABC) technology demonstrator.The 23 January ground test follows three flight tests in which Sikorsky expanded the compound helicopter’s flight envelop to 30kt forward speed with the propulsor disconnected. First flight of the LHTEC T800-801-powered helicopter occurred on 27 August.
